Title page for ETD etd-11182008-063206

A computational study of the 3D flow and performance of a vaned radial diffuser

Degree

Master of Science

Department

Mechanical Engineering

Advisory Committee

Advisor Name

Title

Moore, John

Committee Chair

Dancey, Clinton L.

Committee Member

Ng, W. F.

Committee Member

Keywords

vaned

CFD

diffuser

Date of Defense

1996-08-14

Availability

restricted

Abstract

A computational study was performed on a vaned radial diffuser using the MEFP
(The Moore Elliptic Flow Program) flow code. The vaned diffuser studied by Dalbert et
al. was chosen as a test case for this thesis. The geometry and inlet conditions were
established from this study. The performance of the computational diffuser was compared
to the test case diffuser. The CFD analysis was able to demonstrate the 3D flow within
the diffuser.

An inlet conditions analysis was performed to establish the boundary conditions at
the diffuser inlet. The given inlet flow angles were reduced in order to match the specified
mass flow rate. The inlet static pressure was held constant over the height of the diffuser.

The diffuser was broken down into its subcomponents to study the effects of each
component on the overall performance of the diffuser. The diffuser inlet region, which
comprises the vaneless and semi-vaneless spaces, contains the greatest losses, 56%, but
the highest static pressure rise, 54%. The performance at the throat was also evaluated
and the blockage and pressure recovery were calculated.

The results show the static pressure comparison for the computational study and the test case. The overall pressure rise of the computational study was in good agreement
with the measured pressure rise. The static pressure and total pressure loss distributions in
the inlet region, at the throat, and in the exit region of the diffuser were also analyzed.
The flow development was presented for the entire diffuser. The 3D flow calculations
were able to illustrate a leading edge recirculation at the hub, caused by an inlet skew and
high losses at the hub, and the secondary flows in the diffuser convected the high losses.

The study presented in this thesis demonstrated the flow development in a vaned
diffuser and its subcomponents. The performance was evaluated by calculating the static
pressure rise, total pressure losses, and throat blockage. It also demonstrated current
CFD capabilities for diffusers using steady 3D flow analysis.